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英語人>網(wǎng)絡(luò)例句>wing 相關(guān)的網(wǎng)絡(luò)例句
wing相關(guān)的網(wǎng)絡(luò)例句
與 wing 相關(guān)的網(wǎng)絡(luò)例句 [注:此內(nèi)容來源于網(wǎng)絡(luò)免费。色婬,僅供參考]

A rotor structure for a rotating wing aircraft having substantially rigid rotor head means and rotor blades or wing means arranged in at least one pair, comprising blade angle bearing means (10, 12, 14, 16) for each rotor blade means, tension bar means (6,8) operatively interconnecting the rotor blade means of a pair which blade means are arranged diametrically opposite each other, said tension bar means having a high bending resistance, whereby transmission of bending moments from the rotor blades to the rotor head means is substantially prevented, each of said blade angle bearing means comprising a structure angularly movable in the wing flap direction and in the wing lead-lag direction, at least one of said blade angle bearing means of a pair comprising means permitting an axial motion of the respective tension bar means supported in said blade angle bearing means, and wherein said blade angle bearing means (10, 12, 14, 16) operatively support said tension bar means (6, 8) on said rotor head means (4) for pitch angle rotation of said tension bar means relative to said rotor head means (4), said rotor structure further comprising means (24) securing said rotor blade means (18) to said tension bar means (6, 8) in a manner rigid against rotation of the blade means about the longitudinal blade axis whereby the securing means prevent flapping, drag and lagging movements of the tension bar means, said tension bar means being constructed as torsion bars which are elastic relative to torsion about said longitudinal blade axis.

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A rarer type of aircraft that is neither fixed-wing nor rotary-wing is an ornithopter. A heliplane is both fixed-wing and rotary-wing.

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Others are wing planform (rectangular, tapered, etc.), wing tips, wing twist (we will discuss this topic, as it seems to be one that is frequently misunderstood or underestimated), wing aspect ratio, or span loading (which seems to be overestimated).

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Ln this paper the effect of the position and planform of the canard wing on the burst process of the leading edge vortices over thedouble delta wing and the aerodynamic characteristics of the fighterconfiguration with the double delta wing are presented Furthermore,optimum fighter with the canard-double delta wing has been given.

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Wing Hang opened the breadth of mind,廣納Wuhusihai of brothers and sisters, and "create value for customers," the common aspiration of Wing Hang voluntarily do this strong point, in this atmosphere of everyone should be improved and the distillation of all the Wing Hang people unite closely around the banner of Wing Hang, a firm Hammer, will be able to release the same as the strength of the mountains, we can ensure that this strong point of stability and continuity.

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It is revealed that in comparison of the rigid wing case, the wing deformation acceleration in the flexible wing case leads to the added inertial effect which causes a lot of change in instantaneous aerodynamic performance of the wing.

由柔性翼和剛性翼的結(jié)果比較發(fā)現(xiàn)最新在线观看精品国产福利片,附加慣性效應(yīng)是動態(tài)變形影響氣動性能的主要原因三级片视频网站进入,變形加速率決定了瞬時氣動性能改變量的大小,相比之下性爱综合,動態(tài)變形對氣動性能時均值的影響則弱得多又黄又露又湿又爽的视频。

My main research work is listed as follows: 1. Considering structure characteristics of high aspect ratio flexible wing, features of flat-straight-wing and backswept wing, the aeroelasticity of high aspect ratio of flexible wing, its structure model and aeroelastic dynamics equation of flexible wing have been studied.

針對大展弦比柔性機翼的結(jié)構(gòu)特征,并考慮到平直機翼和后掠機翼的特點性无码视频网站,對大展弦比機翼的氣動彈性進(jìn)行分析性久久久久久久久,分別建立其結(jié)構(gòu)模型,并推導(dǎo)出柔性機翼氣動彈性的動力學(xué)方程网站久久精品。

We have developed many kinds of optical methods to measure the insect flight. For example, a beating force measurement method reduces the uncertainty caused by air turbulence; a flow measurement using a frame straddling technique decreases the interval between exposures of the flow;extracting the weak distorted fringes on the dragonfly wing by a correlation algorithm; measuring the camber deformation of a dragonfly wing using projected comb fringe without hypothesizing that the wing is a rigid plate. By measuring the beating force, wing kinematics and flow, simutantously, we can analyze the relationship among many flight parameters.

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Calibration tool storage cabinet rolling rack w/lights statu go rack rolling rack w/hardhats.tool.rarts metal work station office chairs 7"miter band saw fiberglass backing plates 12"band saw filing cabinets 7 air conditioners 6 humidifiers 2 grinders 2-carts w/testing equipment golf cart 6 utility carts left upper wing right upper wing 4 rolls of final bagging disassembled lay up room lexan 4*8*9/8 3 roof top air ducts preforming core fuselage to wing part non conforming steel/alominum insulation tubes left lower wing right lower wing horizontal upper tail 2 sheets of 1honeycomb core office cubicles cabin door frame template 1 medium size cabinet 2 small cabinets flammable container L.H.boom inboard flap hinge(2) R.H.boom inboard flap hinge(1) L.H.outboard nacelle little fuse CSL mold AFT keelgusset mold LH boom inboard mold RH boom outboard mold LH upper fuel tank mold RH lower fuel tank mold universal safety mats(13) aileron bond/drill jigs metal saw hooses 5-lay up tables safety mat trim kit empty rack office chairs left assembled boom right assembled boom utility carts small file cab bagging material black med.

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Wing architecture is rooted in the model-view-controller design that dates back to SmallTalk.

wing 結(jié)構(gòu)的來源要追溯到 SmallTalk 的模型-視圖-控制者設(shè)計。

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相關(guān)中文對照歌詞
Broken Wing
Kickin' Wing, Animal Doctor
Wing And A Prayer
Death's Great Black Wing Scrapes The Air
Word On A Wing
Little Wing
Little Wing
Chicken Wing
Little Wing
On The Wing
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In the negative and interrogative forms, of course, this is identical to the non-emphatic forms.

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Go down on one's knees;kneel down

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